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Development of multidisciplinary design tools for rapid concept design for aero engine components


Open Rotor engine concepts are strong candidates for future aircraft propulsion. Since many engine architectures options exist, it is of critical importance to quantitatively compare and assess the value of a wide range of alternative concepts with respect to their performance and functionality as well as their impact on risk and cost of realization before down-selection. This CfP aims at developing multidisciplinary tools for structural engine components with specific focus on methods analyzing manufacturing tools’ geometrical accessibility. Please refer to the full topic descriptions document published in this call.